CN113551445A - Airborne evaporation air duct and airborne auxiliary cooling system - Google Patents

Airborne evaporation air duct and airborne auxiliary cooling system Download PDF

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Publication number
CN113551445A
CN113551445A CN202110950892.1A CN202110950892A CN113551445A CN 113551445 A CN113551445 A CN 113551445A CN 202110950892 A CN202110950892 A CN 202110950892A CN 113551445 A CN113551445 A CN 113551445A
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China
Prior art keywords
air
guide
wind
air duct
evaporation
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CN202110950892.1A
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Chinese (zh)
Inventor
蔡正永
徐如好
赵桓
刘茂龙
陈永杰
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Gree Electric Appliances Inc of Zhuhai
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Gree Electric Appliances Inc of Zhuhai
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Application filed by Gree Electric Appliances Inc of Zhuhai filed Critical Gree Electric Appliances Inc of Zhuhai
Priority to CN202110950892.1A priority Critical patent/CN113551445A/en
Publication of CN113551445A publication Critical patent/CN113551445A/en
Pending legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B39/00Evaporators; Condensers
    • F25B39/02Evaporators
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D13/08Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2339/00Details of evaporators; Details of condensers
    • F25B2339/02Details of evaporators

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Devices For Blowing Cold Air, Devices For Blowing Warm Air, And Means For Preventing Water Condensation In Air Conditioning Units (AREA)

Abstract

The application provides an airborne evaporation wind channel and an airborne auxiliary cooling system. This machine carries evaporation wind channel includes the wind channel body and sets up at this internal wind-guiding drainage blade in wind channel, the bottom of wind channel body is provided with the air intake, the top of wind channel body is provided with the air outlet, air outlet department is provided with evaporimeter installation position, wind-guiding drainage blade can set up between evaporimeter installation position and air intake with rotating, when wind-guiding drainage blade is in first rotational position, can block the passageway of wind channel body, and will fall the comdenstion water conservancy diversion to the inner wall of wind channel body on wind-guiding drainage blade, when wind-guiding drainage blade is in the second rotational position, can open the passageway of wind channel body, and carry out the water conservancy diversion to the air current that the air intake got into. According to the airborne evaporation air duct, condensed water can be prevented from being directly discharged from the air inlet of the evaporation air duct, and the drainage effect of the condensed water is improved.

Description

Airborne evaporation air duct and airborne auxiliary cooling system
Technical Field
The application relates to the technical field of aircraft air conditioners, in particular to an airborne evaporation air duct and an airborne auxiliary cooling system.
Background
The on-board air conditioning system can be subdivided into an external ram air intake via the aircraft engine, a main air conditioning system which is expanded and conditioned to the desired temperature via the aircraft air conditioning system (environmental control system), and an auxiliary cold air conditioning system which conditions the air inside the aircraft for auxiliary conditioning. The two different air streams are conditioned to form air streams with different temperatures, different humidities and different flow rates, and the air streams are mixed and sent to areas needing air conditioning, such as passenger cabins, cargo warehouses and accessory areas of the aircraft.
The airborne auxiliary cooling system is the only cooling system before the takeoff of the airplane, and is different from an airplane environment control system, and the airborne auxiliary cooling system adopts a conventional fluorine refrigeration scheme such as a compressor, a heat exchanger and the like. The air conditioning system is limited by the layout of the airplane, all parts of the air conditioning system are located at different positions of the airplane, and a modular assembly scheme is adopted, so that the air conditioning system is convenient to sell after. Therefore, the auxiliary cooling air conditioning system comprises a compressor unit, a condensation air duct unit, an evaporation unit, a controller unit and the like, and the units are connected by adopting quick connectors.
For the evaporation unit, it is including the evaporimeter, and in the in-process of evaporimeter work, the evaporimeter temperature is lower, constantly forms the comdenstion water, then frosts and blocks up the evaporimeter and lead to the air can't cool down through the evaporimeter. For a refrigeration system, common methods of discharging condensed water are: gravity flow method, water seal method, mechanical lift method, however because the flight state of aircraft can change, when being in different flight states, inclination can change, and when being in some inclination scope, the comdenstion water can be followed the middle part drippage of evaporimeter, directly flies out from the air intake in evaporation wind channel, enters into other positions of aircraft, leads to the drainage effect of comdenstion water relatively poor.
Disclosure of Invention
Therefore, the technical problem that this application will be solved lies in providing an airborne evaporation wind channel and airborne auxiliary cooling system, can avoid the direct air intake discharge from the evaporation wind channel of comdenstion water, improves the drainage effect of comdenstion water.
In order to solve the problems, the application provides an airborne evaporation air duct, including the wind channel body and setting at this internal wind-guiding drainage blade of wind channel, the bottom of wind channel body is provided with the air intake, the top of wind channel body is provided with the air outlet, air outlet department is provided with evaporimeter installation position, wind-guiding drainage blade can set up between evaporimeter installation position and air intake with rotating, when wind-guiding drainage blade is in first rotational position, can block the passageway of wind channel body, and will fall on the inner wall of comdenstion water conservancy diversion to the wind channel body on wind-guiding drainage blade, when wind-guiding drainage blade is in the second rotational position, can open the passageway of wind channel body, and carry out the water conservancy diversion to the air current that the air intake got into.
Preferably, the wind guide and flow guide blade is arranged on one side of the air duct body close to the evaporator installation position.
Preferably, the air guide and flow guide blade can open the channel of the air duct body under the action of wind when the air inlet enters the air, and can block the channel of the air duct body under the action of gravity when the air inlet does not enter the air.
Preferably, the two opposite side walls of the air duct body are provided with mounting seats, and two ends of the air guide and drainage blade can be rotatably mounted on the mounting seats through rotating shafts.
Preferably, wind-guiding drainage blade is at least two, and wind-guiding drainage blade is including the overlap joint end that is located the gravity end of pivot first side and is located the pivot second side, and wind-guiding drainage blade's gravity end overlap joint is served at the overlap joint of adjacent wind-guiding drainage blade in proper order.
Preferably, the width of the gravity end in the radial direction of the rotation shaft is 3 to 10 times the width of the overlapping end in the radial direction of the rotation shaft.
Preferably, the wind guide and guide blades are overlapped together to form a closed guide inclined plane.
Preferably, the diversion inclined plane is a plane; or a diversion trench is formed between the gravity end and the lap joint end of the adjacent wind guide and drainage blades, and the diversion trench inclines downwards.
Preferably, the guide surface of the air guide and drainage blade is rectangular, and the section of the air guide and drainage blade is streamline.
Preferably, the wind guide and flow guide blade is of a hollow structure.
Preferably, the wind guide and drainage blade is made of light materials; and/or the wind guide and drainage blade is integrally formed.
Preferably, still be provided with spacing boss on the lateral wall of wind channel body, spacing boss is located wind-guiding drainage blade's rotation path, and the height phase-match of the height of spacing boss and mount pad, wind-guiding drainage blade can the overlap joint on spacing boss.
Preferably, the mounting seat comprises a projection and a buckle arranged on the projection, and the rotating shaft can be rotatably mounted in the buckle.
Preferably, the snap is provided with a V-shaped guide at the opening.
Preferably, the rotating shaft is provided with an annular groove, and the buckle is clamped in the annular groove.
Preferably, the air inlet is provided with an annular stop structure, the annular stop structure is used for stopping condensate water flowing through the inner wall of the air duct body, and a drain hole is formed in the bottom of the air duct body close to the annular stop structure.
Preferably, the air inlet is circular and the air outlet is rectangular.
Preferably, an included angle of 45-75 degrees is formed between the air inlet direction of the air inlet and the air outlet direction of the air outlet.
Preferably, the air duct body between the air inlet and the air outlet is in smooth transition.
According to another aspect of the application, an onboard auxiliary cooling system is provided, which comprises an onboard evaporation air duct, wherein the onboard evaporation air duct is the onboard evaporation air duct.
The application provides an airborne evaporation wind channel, including wind channel body and the wind-guiding drainage blade of setting in this internal wind channel, the bottom of wind channel body is provided with the air intake, the top of wind channel body is provided with the air outlet, air outlet department is provided with evaporimeter installation position, wind-guiding drainage blade can set up between evaporimeter installation position and air intake with rotating, when wind-guiding drainage blade is in first rotational position, can block the passageway of wind channel body, and will fall the comdenstion water conservancy diversion to the inner wall of wind channel body on wind-guiding drainage blade, when wind-guiding drainage blade is in the second rotational position, can open the passageway of wind channel body, and carry out the water conservancy diversion to the air current that the air intake got into. When the evaporation fan operates, the air guide drainage blade opens the channel of the air channel body and plays a role in guiding air flow entering the air channel from the air inlet, so that the air flow distribution on the surface of the evaporator is more uniform, when the air guide drainage blade seals the channel of the air channel body, the condensed water dropping on the evaporator falls on the air guide drainage blade and cannot directly flow out from the air inlet, and the condensed water can be prevented from being directly discharged from the air inlet of the evaporation air channel, the drainage effect of the condensed water is improved.
Drawings
FIG. 1 is a schematic perspective view of an airborne evaporative duct according to an embodiment of the present application;
FIG. 2 is a schematic top view of an airborne evaporative duct according to one embodiment of the present application;
FIG. 3 is a schematic cross-sectional view of an airborne evaporative duct according to an embodiment of the present application;
FIG. 4 is an enlarged schematic view of FIG. 3 at C;
FIG. 5 is a first state block diagram of an airborne evaporative duct according to one embodiment of the present application;
FIG. 6 is an enlarged view of the structure at D in FIG. 5
FIG. 7 is a second state block diagram of an airborne evaporative duct according to one embodiment of the present application;
fig. 8 is a perspective view of an air guiding and guiding blade of an airborne evaporation duct according to an embodiment of the present application;
fig. 9 is a schematic structural diagram of an air guiding and guiding blade of an airborne evaporation duct according to an embodiment of the present application.
The reference numerals are represented as:
1. an air duct body; 2. wind guiding and guiding blades; 3. an air inlet; 4. an air outlet; 5. an evaporator mounting location; 6. a rotating shaft; 7. a gravity end; 8. a lap joint end; 9. a limiting boss; 10. a bump; 11. buckling; 12. An annular groove; 13. a V-shaped guide portion; 14. an annular stop structure; 15. and (4) draining the water.
Detailed Description
Referring to fig. 1 to 9 in combination, according to an embodiment of the present application, an airborne evaporation air duct includes an air duct body 1 and air guide and drainage blades 2 disposed in the air duct body 1, an air inlet 3 is disposed at the bottom of the air duct body 1, an air outlet 4 is disposed at the top of the air duct body 1, an evaporator mounting position 5 is disposed at the air outlet 4, the air guide and drainage blades 2 can be rotatably disposed between the evaporator mounting position 5 and the air inlet 3, when the air guide and drainage blades 2 are in a first rotation position, a channel of the air duct body 1 can be blocked, condensed water falling on the air guide and drainage blades 2 is guided to an inner wall of the air duct body 1, when the air guide and drainage blades 2 are in a second rotation position, the channel of the air duct body 1 can be opened, and air flow entering from the air inlet 3 is guided.
The airborne evaporation air duct is provided with the air guide and drainage blade 2 at the lower side of an evaporator installation position 5 for installing an evaporator, the air guide and drainage blade 2 can rotate, the effect of the air guide and drainage blade 2 can be adjusted by adjusting the rotating position of the air guide and drainage blade 2, the air guide and drainage blade 2 seals a channel of the air duct body 1 after the evaporation fan is closed, condensed water on the evaporator is drained to the inner wall of the air duct along the surface of the air guide and drainage blade 2 and is discharged after being collected to the bottom of the air duct, when the evaporation fan operates, the air guide and drainage blade 2 opens the channel of the air duct body 1, and the air flow entering the air duct from the air inlet 3 is guided, so that the air flow on the surface of the evaporator is more uniformly distributed, and the heat exchange efficiency is higher; when wind-guiding drainage blade 2 blocks the passageway of wind channel body 1, the comdenstion water that drips on the evaporimeter can fall on wind-guiding drainage blade 2, and unable direct from air intake 3 flows, consequently can avoid the comdenstion water to directly discharge from air intake 3 in evaporation wind channel, improves the drainage effect of comdenstion water.
This application is through setting up wind-guiding drainage blade 2 to make wind-guiding drainage blade 2 have different rotational position, the drainage demand of any flight gesture when can solving aircraft normal flight, the drainage is more reliable.
In one embodiment, the wind-guiding and flow-guiding blade 2 is arranged on one side of the air duct body 1 close to the evaporator installation position 5, so that the distance from the evaporator to the surface of the wind-guiding and flow-guiding blade 2 can be shortened, and the dropping noise of the condensed water can be reduced.
In one embodiment, the wind guiding and guiding blade 2 can open the channel of the air duct body 1 under the action of wind when the wind enters the wind inlet 3, and block the channel of the air duct body 1 under the action of gravity when the wind does not enter the wind inlet 3. In this embodiment, the rotation control of the wind guide and guide vanes 2 is controlled by wind power and self gravity, so that an additional power mechanism is not needed, and the wind guide and guide vanes 2 can be automatically opened under the action of the wind power when the wind enters the air inlet 3, so that the problem that the bottom of the evaporator is uneven and low in efficiency due to the fact that the bottom of the evaporator is blocked by the air flow in the bottom of the evaporator in the related art can be effectively solved.
In other embodiments, the air guiding vane 2 may be connected to a driving mechanism, and the driving mechanism controls the operation position of the air guiding vane 2. The drive mechanism is, for example, a drive motor. Adopt actuating mechanism driven mode to carry out wind-guiding drainage blade 2's rotational position control, can realize the active control to wind-guiding drainage blade 2's rotational position, control is more accurate, and can force the position restriction to wind-guiding drainage blade 2 when needing, can effectively satisfy wind-guiding drainage blade 2's special control demand.
In order to avoid interference between the wind guide and drainage blades 2 and the evaporator in the rotating process, the distance between the wind guide and drainage blades 2 and the bottom of the evaporator should be greater than the height of the wind guide and drainage blades 2 when the wind guide and drainage blades 2 are completely erected.
The air outlet of the onboard evaporation air duct is provided with a mounting surface for mounting the evaporator, the mounting surface is provided with a folded plate which is folded towards the periphery, the folded plate is provided with a mounting hole, the evaporator is provided with a mounting side edge, the mounting side edge of the evaporator is also provided with a mounting hole, and after the mounting hole on the mounting side edge of the evaporator is aligned with the mounting hole on the folded plate, the evaporator is connected through a screw, so that the evaporator is mounted in the evaporator mounting position 5. Because the evaporimeter passes through the folded plate and installs fixedly, consequently the evaporimeter is located the part of evaporimeter installation position 5 and can be unsettled, need not to set up bearing structure etc. can not form the hindrance to the air inlet side of evaporimeter, consequently can increase the heat transfer area of evaporimeter more effectively, improves the heat exchange efficiency of evaporimeter.
Be provided with the business turn over pipe fixed orifices on the lateral wall of evaporimeter installation position 5, be provided with the concave groove on the business turn over pipe fixed orifices, be provided with the rubber ring on the business turn over pipe, the rubber ring is installed in the concave groove to realize the sealing connection between the business turn over pipe of evaporimeter installation position 5 and evaporimeter.
In a real time, the two opposite side walls of the air duct body 1 are provided with mounting seats, and the two ends of the air guide and guide vanes 2 can be rotatably mounted on the mounting seats through the rotating shaft 6. Can be fixed connection between pivot 6 and the wind-guiding drainage blade 2, also can be for rotating relatively and connecting, when being fixed connection between pivot 6 and the wind-guiding drainage blade 2, rotate between pivot 6 and the mount pad and be connected to guarantee that wind-guiding drainage blade 2 can the free rotation, realize opening or close the control of passageway, when being connected for rotating between pivot 6 and the wind-guiding drainage blade 2, can be for rotating between pivot 6 and the mount pad and be connected, also can be fixed connection.
In one embodiment, the number of the wind guide and guide blades 2 is at least two, the wind guide and guide blades 2 comprise a gravity end 7 positioned on a first side of the rotating shaft 6 and a lap end 8 positioned on a second side of the rotating shaft 6, and the gravity end 7 of the wind guide and guide blade 2 is overlapped on the lap end 8 of the adjacent wind guide and guide blade 2 in sequence.
In this embodiment, the windward area of the gravity end 7 is greater than the windward area of the lap end 8, so that when the air enters the air inlet 3, the wind force acting on the gravity end 7 is greater than the wind force acting on the lap end 8, the channel of the evaporation air channel is smoothly opened, and smooth flow guiding of the air flow is realized. As a preferred embodiment, the frontal area of the gravity end 7 is more than 3 times the frontal area of the overlap end 8.
Gravity end 7's gravity will be greater than overlap joint end 8's gravity to guarantee when air intake 3 is not intake, overlap joint end 8's gravity can be overcome to gravity end 7's gravity, thereby the whereabouts, realize with the overlap joint of adjacent wind-guiding drainage blade 2's overlap joint end 8, and then the passageway in closed evaporation wind channel.
In one embodiment, in order to ensure the windward side of the gravity end 7 and avoid the problem that the width of the gravity end 7 is too wide to form large gravity, which affects the smooth driving of wind power, the width of the gravity end 7 in the radial direction of the rotating shaft 6 is 3 to 10 times of the width of the overlapping end 8 in the radial direction of the rotating shaft 6.
In one embodiment, the wind guide and guide blades 2 are overlapped together to form a closed guide inclined plane, so that condensed water can flow to the inner wall of the air duct along the continuous guide inclined plane and then flow to the water discharge hole 15 at the bottom of the airborne evaporation air duct under the action of gravity to be discharged.
In one embodiment, the diversion inclined plane is a plane, so that better flowing continuity of the condensed water is ensured. In this embodiment, the lower surface of the gravity end 7 and the upper surface of the lap end 8 need to be specially designed, so that the lower surface of the gravity end 7 has a structure matched with the upper surface of the lap end 8 at a position matched with the upper surface of the lap end 8, and the gravity end 7 and the lap end 8 are well attached together, so that the upper surface of the gravity end 7 and the upper surface of the lap end 8 are in contact at a joint position and have the same height.
In one embodiment, a diversion trench is formed between the gravity end 7 and the overlapping end 8 of the adjacent wind guide and guide blades 2, and the diversion trench is inclined downwards. In this embodiment, the wind-guiding and guiding blade 2 may be inclined or horizontal in the width direction, and when the water flow reaches the diversion trench, the water flow flows to the inner wall of the air duct along the diversion trench, and then flows downward along the inner wall of the air duct.
In one embodiment, the flow guide surface of the wind guide and flow guide blade 2 is rectangular, and the cross section of the wind guide and flow guide blade 2 is streamline, so that the wind resistance can be effectively reduced, and the flow guide effect is improved.
In one embodiment, the wind guide and guide blade 2 is a hollow structure. In this embodiment, the hollow structure of the wind guide and guide blade 2 can reduce the weight of the wind guide and guide blade 2, so that a larger windward side can be obtained under the condition that the wind guide and guide blade 2 has a lighter weight, and the wind guide and guide blade can be better driven by the airflow of the air inlet 3. The hollow structure of the wind guide and drainage blade 2 is a totally enclosed structure, so that condensed water is prevented from entering, and influence on air outlet efficiency caused by air flow entering is avoided.
In one embodiment, the upper surface and the lower surface of the gravity end 7 intersect at a sharp angle, i.e., the angle formed by the intersection of the upper surface and the lower surface is less than or equal to 20 °, thereby reducing the resistance to airflow and reducing the overall thickness of the gravity end 7 after overlapping the overlapping end 8.
In one embodiment, the air guiding and guiding blade 2 is made of a light material, so that the weight of the air guiding and guiding blade 2 can be reduced, and the air guiding and guiding blade 2 can be more easily blown by airflow.
In one embodiment, the wind guide and guide vane 2 is integrally formed, and the structural integrity is better.
Wind-guiding drainage blade 2 can adopt combined material or aluminum alloy to print integrated into one piece through 3D.
In one embodiment, a limiting boss 9 is further arranged on the side wall of the air duct body 1, the limiting boss 9 is located on a rotation path of the air guiding and guiding blade 2, the height of the limiting boss 9 is matched with the height of the mounting seat, and the air guiding and guiding blade 2 can be lapped on the limiting boss 9. In this embodiment, spacing boss 9 is located a lateral wall of wind channel body, and be located the motion path of the tip position of the gravity end 7 of the wind guide drainage blade 2 that is closest to spacing boss 9, can form the support to gravity end 7 when the gravity end 7 of this wind guide drainage blade 2 falls, make other wind guide drainage blade 2 all can form the support through this wind guide drainage blade 2, thereby guarantee that all blade supports upwards open, and can not open downwards, the orderly work of wind guide drainage blade 2 has been guaranteed.
Other wind-guiding drainage blade 2 and the wind-guiding drainage blade 2 of this position department overlap joint screens installation in proper order to make the wind-guiding drainage blade 2 after installing smoothly open, and can not touch the evaporimeter lower surface when opening, can form a confined inclined plane at the evaporimeter lower surface after closing.
In one embodiment, the mounting seat comprises a projection 10 and a catch 11 arranged on the projection 10, the shaft 6 being rotatably mounted in the catch 11. In this embodiment, the mount pad setting can be an integral structure on two relative lateral walls in evaporation wind channel, and the mount pad of same one side also can be a buckle 11 and correspond a mount pad, and buckle 11 sets up at the both ends of pivot 6, can install spacingly to pivot 6. The buckle 11 is the round hole structure, and the top has the opening, makes things convenient for pivot 6 to carry on spacingly after going into, can not restrict pivot 6's rotation after pivot 6 cards are gone into simultaneously.
In one embodiment, the catch 11 is provided with a V-shaped guide 13 at the opening. The V-shaped guide part 13 has an upward opening, so that guide can be formed for the installation of the rotating shaft 6, the installation difficulty of the rotating shaft 6 is reduced, and the installation efficiency is improved.
The bottom of mount pad and wind channel inner wall transition are even, can reduce the resistance of mount pad, improve the smooth and easy nature that the air current flows.
In one embodiment, the rotating shaft 6 is provided with an annular groove 12, the buckle 11 is clamped in the annular groove 12, and the axial limit of the rotating shaft 6 can be realized by utilizing the cooperation of the annular groove 12 and the buckle 11.
In one embodiment, an annular stop structure 14 is disposed at the air inlet 3, the annular stop structure 14 is used for stopping the condensed water flowing through the inner wall of the air duct body 1, and a drain hole 15 is disposed at a bottom position of the air duct body 1 near the annular stop structure 14. In this embodiment, annular backstop structure 14 forms the return water bay in air intake position department, can need not to set up the water collector and realize the collection to the comdenstion water, and annular backstop structure 14's bottom sets up wash port 15, can in time pass through wash port 15 with the comdenstion water that the return water bay was collected and discharge. The drain holes 15 are circular drain holes, and the number of the drain holes is not limited, so that the requirement of draining water in extreme cases can be met. The other end of the drain hole 15 is connected to a drain pipe, which can guide the condensed water to a specific position of the airplane.
In one embodiment, the intake opening 3 is circular and the outlet opening 4 is rectangular. The operation air inlet 3 is adopted, a backwater bay for collecting condensate water from the inner surface of the air channel can be conveniently designed around the air inlet, and the rectangular air outlet 4 is adopted, so that the rectangular evaporator can be better adapted.
In one embodiment, an included angle of 45 degrees to 75 degrees is formed between the air inlet direction of the air inlet 3 and the air outlet direction of the air outlet 4.
The air duct body 1 between the air inlet 3 and the air outlet 4 is in smooth transition.
Preferably, the two air ports form an included angle of 60 degrees, and the middle parts of the two air ports are in smooth transition connection, so that the air resistance of the air duct is small, and the air flow distribution on the heat exchange surface of the evaporator is more uniform.
When the air conditioning system needs to remove water and frost, the evaporation fan is closed, the air guide and drainage blade 2 is closed under the action of gravity, before the aircraft takes off or flies flatly, the air inlet 3 of the airborne evaporation air duct is right opposite to the right, the air inlet plane of the air inlet 3 is a vertical plane, the aircraft head faces horizontally, as shown in fig. 5, the schematic diagram of the position of the evaporation air duct is shown when the aircraft head faces downwards for 45-degree extreme conditions, the evaporation air duct is used for simulating water drainage under extreme conditions, the air duct is in a position which is more favorable for water drainage under normal flight postures of other aircraft, and only the water drainage scheme under the extreme conditions is introduced. After the defrosting working condition is started, the evaporation fan stops, the wind guide and drainage blades 2 are closed under the action of gravity and are sequentially overlapped to form a closed inclined plane. The comdenstion water separates from the evaporator lower surface under the action of gravity, and the condensation water in middle part drips behind the closed inclined plane that is formed by wind-guiding drainage blade 2, flows to the wind channel inner wall at spacing boss 9 place under the action of gravity, or the certain wind channel inner wall aircraft slope of mount pad place, and with other comdenstion water that drip the wind channel inner wall together, along the wind channel inner wall down collect bottom return water bay, discharge through wash port 15.
After defrosting is completed, condensate water on the surface of the evaporator is drained, the evaporation fan is opened at the moment, the wind guide and drainage blade 2 is opened under the action of wind power, and the state of the evaporation air channel assembly is shown in a figure 7. Under the action of an evaporation fan, the air guide and drainage blades 2 are positioned at the position vertically upward along the wind direction, air in the engine room is sucked through the air inlet 3 of the air duct, sequentially passes through the flow guide channels of the air guide and drainage blades 2, and is cooled by flowing through the evaporator and then is conveyed to the engine room through the air pipe.
According to the embodiment of the application, the onboard auxiliary cooling system comprises an onboard evaporation air duct which is the onboard evaporation air duct.
It is readily understood by a person skilled in the art that the advantageous ways described above can be freely combined, superimposed without conflict.
The present invention is not intended to be limited to the particular embodiments shown and described, but is to be accorded the widest scope consistent with the principles and novel features herein disclosed. The foregoing is only a preferred embodiment of the present application, and it should be noted that, for those skilled in the art, several modifications and variations can be made without departing from the technical principle of the present application, and these modifications and variations should also be considered as the protection scope of the present application.

Claims (20)

1. An airborne evaporation air duct is characterized by comprising an air duct body (1) and air guide and drainage blades (2) arranged in the air duct body (1), wherein an air inlet (3) is arranged at the bottom of the air duct body (1), an air outlet (4) is arranged at the top of the air duct body (1), an evaporator installation position (5) is arranged at the air outlet (4), the air guide and drainage blades (2) can be rotatably arranged between the evaporator installation position (5) and the air inlet (3), when the air guide and drainage blades (2) are in a first rotating position, a channel of the air duct body (1) can be blocked, condensed water falling on the air guide and drainage blades (2) is guided to the inner wall of the air duct body (1), and when the air guide and drainage blades (2) are in a second rotating position, the channel of the air duct body (1) can be opened, and guides the air flow entering from the air inlet (3).
2. The airborne evaporation air duct of claim 1, characterized in that the air guide and guide vanes (2) are arranged on one side of the air duct body (1) close to the evaporator mounting position (5).
3. The onboard evaporation air duct according to claim 1, wherein the air guide and guide vanes (2) can open the passage of the air duct body (1) under the action of wind when the air inlet (3) enters air, and block the passage of the air duct body (1) under the action of gravity when the air inlet (3) does not enter air.
4. The airborne evaporation duct of claim 1, characterized in that the duct body (1) is provided with mounting seats on two opposite side walls, and the wind guide and guide vanes (2) are rotatably mounted on the mounting seats through rotating shafts (6) at two ends.
5. The airborne evaporation duct of claim 4, characterized in that, the number of the wind-guiding and guiding vanes (2) is at least two, the wind-guiding and guiding vanes (2) comprise a gravity end (7) at the first side of the rotating shaft (6) and a lap end (8) at the second side of the rotating shaft (6), and the gravity end (7) of the wind-guiding and guiding vanes (2) is overlapped on the lap end (8) of the adjacent wind-guiding and guiding vanes (2) in sequence.
6. The airborne evaporation duct of claim 5, characterized in that the width of the gravity end (7) in the radial direction of the rotating shaft (6) is 3 to 10 times the width of the overlap end (8) in the radial direction of the rotating shaft (6).
7. The airborne evaporation duct of claim 5, characterized in that the wind-guiding and guiding vanes (2) are lapped together to form a closed guiding inclined plane.
8. The on-board evaporative duct of claim 7, wherein the deflector ramp is planar; or a diversion trench is formed between the gravity end (7) and the lap joint end (8) of the adjacent wind guide and guide blades (2), and the diversion trench is inclined downwards.
9. The airborne evaporation air duct of claim 3, characterized in that the flow guide surface of the air guide and guide vane (2) is rectangular, and the cross section of the air guide and guide vane (2) is streamlined.
10. The airborne evaporation wind tunnel according to claim 9, characterized in that the wind guiding and guiding blade (2) is of a hollow structure.
11. The onboard evaporation air duct of claim 3, characterized in that said air guiding and guiding blades (2) are made of light material; and/or the wind guide and drainage blades (2) are integrally formed.
12. The airborne evaporation air duct of claim 4, characterized in that a limiting boss (9) is further disposed on the side wall of the air duct body (1), the limiting boss (9) is located on the rotation path of the air guide and guide vanes (2), the height of the limiting boss (9) is matched with the height of the mounting seat, and the air guide and guide vanes (2) can be lapped on the limiting boss (9).
13. The onboard evaporation air duct of claim 4, characterized in that the mounting comprises a lug (10) and a catch (11) provided on the lug (10), the shaft (6) being rotatably mounted in the catch (11).
14. The onboard evaporation air duct according to claim 13, characterized in that said snap (11) is provided with a V-shaped guide (13) at the opening.
15. The onboard evaporation air duct of claim 13, wherein the rotating shaft (6) is provided with an annular groove (12), and the buckle (11) is clamped in the annular groove (12).
16. The onboard evaporation air duct according to claim 1, wherein an annular stop structure (14) is disposed at the air inlet (3), the annular stop structure (14) is used for stopping condensed water flowing through the inner wall of the air duct body (1), and a drain hole (15) is disposed at a bottom position of the air duct body (1) close to the annular stop structure (14).
17. The onboard evaporation air duct according to claim 1, characterized in that said air inlet (3) is circular and said air outlet (4) is rectangular.
18. The airborne evaporation duct of claim 1, wherein an included angle of 45 degrees to 75 degrees is formed between the air inlet direction of the air inlet (3) and the air outlet direction of the air outlet (4).
19. The onboard evaporation air duct according to claim 1, characterized in that the air duct body (1) between the air inlet (3) and the air outlet (4) is in smooth transition.
20. An onboard auxiliary cooling system comprising an onboard evaporation air duct, wherein the onboard evaporation air duct is the onboard evaporation air duct of any one of claims 1 to 19.
CN202110950892.1A 2021-08-18 2021-08-18 Airborne evaporation air duct and airborne auxiliary cooling system Pending CN113551445A (en)

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